View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 17589U 26040.40288984 +.00000000 +00000-0 +51136-4 0 00008
2 17589 70.9215 25.4666 0024901 252.4435 107.3966 14.13056629 05
| Epoch (UTC): | 09 February 2026 09:40:09 |
| Eccentricity: | 0.0024901 |
| inclination: | 70.9215° |
| perigee height: | 831 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 25.4666° |
| argument of perigee: | 252.4435° |
| revolutions per day: | 14.13056629 |
| mean anomaly at epoch: | 107.3966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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